Statics: cram pack

Formula sheets, the key method steps for every topic and 12 practice problems, with full solutions at the back.

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1Formulas and methods

Vectors: dot & cross product

Magnitude
|a| = √(ax² + ay² + az²)
Unit vector
û = a/|a|
Components from an angle
Fx = F·cos θ, Fy = F·sin θ
Dot product
a·b = axbx + ayby + azbz = |a||b|cos θ
Scalar projection of a onto b
a·b/|b|
Work
W = F·d
Cross product
a × b = (aybz − azby, azbx − axbz, axby − aybx)
Areas
parallelogram |a × b|, triangle ½|a × b|
Moment about O
MO = r × F, r = A − O
Volume of a parallelepiped
V = |a·(b × c)|

Method

  1. Write every vector in components; for a force given by a magnitude and an angle, use F·cos θ and F·sin θ.
  2. For lengths and directions use the magnitude √(x² + y² + z²) and the unit vector a/|a|.
  3. Use the dot product for angles, projections, perpendicularity and work: a·b = |a||b|cos θ.
  4. Use the cross product for perpendicular vectors, areas and moments: write the three components carefully, keeping the order a × b.

Beam support reactions

Equilibrium
ΣFx = 0, ΣFy = 0, ΣM = 0
Uniform load
resultant w·L at the middle of the load
Moment
M = F·d

Method

  1. Draw a free-body diagram and replace each support by its reactions.
  2. Replace every distributed load by a single force at its centroid.
  3. Take moments about one support to find the reaction at the other.
  4. Use ΣFy = 0 to find the remaining reaction, and check with a second moment equation.

Truss: method of joints

Method of joints
ΣFx = 0, ΣFy = 0 at each joint
Method of sections
ΣM = 0 about a cut point
Member force
positive = tension, negative = compression

Method

  1. Find the support reactions for the whole truss.
  2. Method of joints: start at a joint with at most two unknown member forces and use ΣFx = 0 and ΣFy = 0.
  3. Method of sections: cut through the member you need and take moments about a point where the other unknown members meet.
  4. Assume tension; a negative answer means compression.

Frames & machines

Equilibrium of each member
ΣFx = 0, ΣFy = 0, ΣM = 0
Two-force member
force along the line through its two pins
Pin force
equal and opposite on the two members it joins
Magnitude of a pin force
F = √(Fx² + Fy²)
Lever, pliers, bell crank
Fin·a = Fout·b
Toggle
Flink = F/(2 sin θ), Q = F/(2 tan θ)
Uniform load
resultant w·L at the middle of the load

Method

  1. Draw the whole structure and find the support reactions if there are no more than three unknowns.
  2. Spot the two-force members: loaded only at two pins, their force acts along the line between the pins.
  3. Take the frame apart and draw every member on its own, with equal and opposite pin forces where members meet.
  4. For each member, take moments about a pin with unknown forces, then use ΣFx = 0 and ΣFy = 0; combine components into a magnitude at the end.

Shear force & bending moment

Shear and moment
V = ΣF on one side, M = ΣF·d on one side
Bending stress
σ = M·y/I
Rectangle
I = bh³/12
Section modulus
W = I/ymax
Simply supported, uniform load
Mmax = wL²/8

Method

  1. Find the support reactions from equilibrium of the whole beam.
  2. Cut the beam at the section you need and keep one side.
  3. Shear force: sum of the vertical forces on that side. Bending moment: sum of their moments about the cut.
  4. For the maximum moment, find where the shear force is zero.

Centroid & second moment of area

Centroid
ȳ = ΣAiyi/ΣAi
Rectangle
I = bh³/12
Parallel-axis theorem
I = Ic + A·d²
Composite section
I = Σ(Ic,i + Aidi²)

2Practice problems

1.Vectors: dot & cross productMedium
xyzab

Find the value of k for which the vectors a = (−4, −6, 6) and b = (k, −3, 4) are perpendicular.

a = (−4, −6, 6)b = (k, −3, 4)
k =
2.Vectors: dot & cross productHard
xyzrFOA

A force F = (10, 50, 50) N acts at point A(4, −1, 2). Coordinates are in metres. Find the y-component My of the moment of the force about the origin O(0, 0, 0).

F = (10, 50, 50) NA(4, −1, 2) mO(0, 0, 0) m
My = N·m
3.Beam support reactionsMedium
P = 65 kNM = 15 kN·mABRA​ = ?3 m1 m6 m

The simply supported beam has a pin at A and a roller at B. It carries a point load P at 4 m from A and a clockwise couple M at 3 m from A. Find the vertical reaction RA, taking upward as positive.

L = 10 mP = 65 kN at 4 mM = 15 kN·m (clockwise) at 3 m
RA = kN
4.Beam support reactionsHard
w = 6 kN/mP = 15 kNABRA​ = ?RB​1 m1.5 m1.5 m

The simply supported beam has a pin at A and a roller at B. Find the vertical support reaction RA.

L = 4 mP = 15 kN at 2.5 mw = 6 kN/m from 1 to 4 m
RA = kN
5.Truss: method of jointsMedium
ABBCACACB30 kN5 m4 m3 m

Use the method of joints to find the force FAC in member AC. Give tension as positive and compression as negative.

span = 5 mheight = 3 mB is 4 m from Avertical load = 30 kN
FAC = kN
6.Truss: method of jointsHard
ABCDEFGH20 kN20 kN30 kN25 kN4 × 4 m3 m

Exactly one member of this truss carries no force under these loads. Which is the zero-force member? Click it in the diagram.

B: 20 kN ↓G: 20 kN ↓H: 30 kN ↓H: 25 kN ←
  1. 1member AB
  2. 2member BC
  3. 3member CD
  4. 4member DE
  5. 5member FG
  6. 6member GH
  7. 7member AF
  8. 8member HE
  9. 9member BF
  10. 10member CG
  11. 11member DH
  12. 12member FC
  13. 13member HC
7.Frames & machinesMedium
OAB80 NQ200 mm120 mmFO​ = ?

The bell crank shown turns about the pin O. A vertical force of 80 N at A (200 mm from O) is balanced by a horizontal force at B (120 mm above O). Find the magnitude of the pin reaction FO.

F = 80 NOA = 200 mmOB = 120 mm
FO = N
8.Frames & machinesHard
15 kN2 kN4 m3 mABC

A uniform horizontal boom AB of weight 2 kN is pinned to a wall at A and held by a cable from B to the point C on the wall, 3 m above A. A load of 15 kN hangs at B. Find the magnitude of the pin reaction A.

W = 15 kNWb = 2 kNAB = 4 mAC = 3 m
A = kN
9.Shear force & bending momentMedium
M0​ = 55 kN·mAB1.5 m4.5 m

The simply supported beam carries a clockwise couple M0 = 55 kN·m at x = 1.5 m from A, and no other load. Find the bending moment Mx just to the left of the couple. Use sagging moments positive and upward shear on the left face positive.

L = 6 mM0 = 55 kN·m clockwise, at 1.5 m
Mx = kN·m
10.Shear force & bending momentHard
w = 10 kN/mP = 20 kNABsection4 m6 m

Find the bending moment Mx at the section x = 4 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 10 mP = 20 kN at 4 mw = 10 kN/m from 0 to 10 mx = 4 m
Mx = kN·m
11.Centroid & second moment of areaMedium
1002510014xdimensions in mm

Find the second moment of area Ix of the T-section about the horizontal axis x through its centroid.

bf = 100 mmtf = 25 mmtw = 14 mmhw = 100 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
260202608xsagging Mdimensions in mm

A cast-iron beam has the T-section shown, with the flange on top. The allowable stresses are 50 MPa in tension and 120 MPa in compression. Find the largest sagging bending moment Mallow the beam can carry.

bf = 260 mmtf = 20 mmtw = 8 mmhw = 260 mmσt,allow = 50 MPaσc,allow = 120 MPa
Mallow = kN·m

3Solutions

1.Vectors: dot & cross product

Answer: k = 10.5

Dot product: a·b = axbx + ayby + azbz = |a|·|b|·cos θ, a scalar. It gives the angle between two vectors, cos θ = a·b/(|a|·|b|), and it is zero when they are perpendicular. The scalar projection of a onto b is a·b/|b|, and a constant force F moving through a displacement d does work W = F·d.

Dot product equals zero

a·b = (−4)·k + (−6)·(−3) + 6·4 = 0
42 + (−4)·k = 0

Solve for k

k = −42/(−4) = 10.5

Answer

k = 10.5
2.Vectors: dot & cross product

Answer: My = −180 N·m

Cross product: a × b = (aybz − azby, azbx − axbz, axby − aybx) is perpendicular to both vectors, and |a × b| = |a|·|b|·sin θ is the area of the parallelogram they span (the triangle has half of it). Order matters: b × a = −(a × b). The moment of a force F applied at point A about point O is MO = r × F, with r = A − O.

Position vector from O to A

r = A − O = (4, −1, 2) − (0, 0, 0) = (4, −1, 2) m

Moment M = r × F

(r × F)x = ryFz − rzFy = (−1)·50 − 2·50 = −150 N·m
(r × F)y = rzFx − rxFz = 2·10 − 4·50 = −180 N·m
(r × F)z = rxFy − ryFx = 4·50 − (−1)·10 = 210 N·m

Requested component

My = −180 N·m

Answer

My = −180 N·m
3.Beam support reactions

Answer: RA = 37.5 kN

Static equilibrium: a body at rest has ΣFx = 0, ΣFy = 0 and ΣM = 0 about any point. Replace each distributed load by its resultant (its area) acting at the centroid of the load diagram, and take moments about a support to remove that support’s reaction from the equation.

Moments about A

Counter-clockwise positive.

ΣMA = 0: RB·10 − 65·4 − 15 = 0
RB = 275/10 = 27.5 kN

Vertical equilibrium

RA = 65 − 27.5 = 37.5 kN

Answer

RA = 37.5 kN

A negative reaction acts downward.

4.Beam support reactions

Answer: RA = 12.38 kN

Static equilibrium: a body at rest has ΣFx = 0, ΣFy = 0 and ΣM = 0 about any point. Taking moments about one support removes that support’s reaction from the equation.

w = 6 kN/mP = 15 kNABRA​RB​1 m1.5 m1.5 m

Free-body diagram

Replace the supports with reaction forces. A roller gives one vertical reaction; with only vertical loads the pin gives one vertical reaction too.

Equilibrium

Moments about A, counter-clockwise positive. Then vertical force balance.

UDL resultant: W = w·ℓ = 6·3 = 18 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·4 = 15·2.5 + 6·3·2.5
RB = 82.5/4 = 20.63 kN
ΣFy = 0: RA = 33 − 20.63 = 12.38 kN

Answer

RA = 12.38 kN
5.Truss: method of joints

Answer: FAC = 8 kN

Method of joints: every pin of a truss is in equilibrium, so ΣFx = 0 and ΣFy = 0 at each joint. Start at a joint with at most two unknown member forces. A negative result means the member is in compression.

ABBCACACB30 kNAy​Cy​

Support reactions

Equilibrium of the whole truss. Moments about A, counter-clockwise positive.

ΣMA = 0: Cy·5 = 30·4 → Cy = 24 kN
ΣFy = 0: Ay = 30 − 24 = 6 kN

Joint C

The roller gives only a vertical reaction, so joint C has just two unknown member forces. Assume both in tension.

sin γ = 3/3.162 = 0.9487, cos γ = 1/3.162 = 0.3162
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −24/0.9487 = −25.3 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−25.3)·0.3162 = 8 kN

Answer

FAC = 8 kN (tension)
6.Truss: method of joints

Answer: member DH

Zero-force members: at a joint, the forces must balance in every direction. If a joint has no load and no support, and two of its three members are in line, then the balance across that line involves only the third member, so its force is zero. If only two members meet at an unloaded joint and they are not in line, both are zero.

Joint D

CD and DE lie on one straight line and the joint carries no load. Balancing forces across that line leaves only DH.

ΣF⊥ = 0 → FDH = 0

Check with the method of joints

Solving all joints gives these member forces (T = tension, C = compression).

AB: 24.58 kN (T), BC: 24.58 kN (T), CD: 43.75 kN (T), DE: 43.75 kN (T), FG: 72.5 kN (C), GH: 72.5 kN (C), AF: 61.98 kN (C), HE: 54.69 kN (C), BF: 20 kN (T), CG: 20 kN (C), DH: 0, FC: 28.65 kN (T), HC: 4.688 kN (T)

Answer

Zero-force member: DH
7.Frames & machines

Answer: FO = 155.5 N

Machines: pliers, levers, linkages and clamps turn an input force into a larger or a differently directed output force. Draw one part as a free body and take moments about its pivot: the pin force drops out, and Fin·a = Fout·b gives the mechanical advantage a/b. The pin force then follows from ΣF = 0 on the same part. In a toggle, two links meet at a shallow angle θ; each link is a two-force member, so a small force F at the joint creates large link forces F/(2 sin θ) and a clamping force F/(2 tan θ).

Force at B

Q = 80·200/120 = 133.3 N

Pin reaction

Ox = 133.3 N, Oy = 80 N
FO = √(133.3² + 80²) = 155.5 N

Answer

FO = 155.5 N
8.Frames & machines

Answer: A = 21.36 kN

Frames and machines: unlike a truss, a frame contains at least one member that carries forces at more than two points, or a load between its pins. First look for two-force members: a member loaded only at two pins has its force along the line through them, so it adds one unknown, not two. Then use the whole structure for the support reactions when there are no more than three unknowns. Finally take the frame apart: draw each member separately, with the pin forces equal and opposite on the two members they connect, and write ΣFx = 0, ΣFy = 0 and ΣM = 0 for it. Taking moments about a pin removes both components of that pin force from the equation.

Cable tension

T = (15 + 2/2)/0.6 = 26.67 kN

Components at A

Ax = T·cos β = 21.33 kN
Ay = 15 + 2 − T·sin β = 1 kN

Magnitude

A = √(21.33² + 1²) = 21.36 kN

Answer

A = 21.36 kN
9.Shear force & bending moment

Answer: Mx = −13.75 kN·m

Method of sections: cut the beam where you want the internal forces and keep one side. The shear force V balances the vertical forces on that side, and the bending moment M balances their moments about the cut. An applied couple makes the bending moment diagram jump by the size of the couple.

Support reactions

Moments about A, counter-clockwise positive: RB·L − M0 = 0. Vertical balance: RA + RB = 0.

RB = M0/L = 55/6 = 9.167 kN (upward)
RA = −RB = −9.167 kN (downward)

Cut just left of the couple

The left part contains only RA.

Mx = RA·a = −9.167·1.5 = −13.75 kN·m

Answer

Mx = −13.75 kN·m
10.Shear force & bending moment

Answer: Mx = 168 kN·m

Method of sections: cut the beam where you want the internal forces and keep one side. The shear force V balances the vertical forces on that side, and the bending moment M balances their moments about the cut.

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 10·10 = 100 kN, acting at x̄ = 5 m
ΣMA = 0: RB·10 = 20·4 + 10·10·5
RB = 580/10 = 58 kN
ΣFy = 0: RA = 120 − 58 = 62 kN
w = 10 kN/mP = 20 kNABRA​ = 62RB​ = 58section4 m6 m

Cut at x = 4 m and keep the left part

Only forces left of the cut appear. A UDL portion acts as one force at the middle of that portion.

M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 62·4 − 10·4·2 = 168 kN·m

Answer

Mx = 168 kN·m
11.Centroid & second moment of area

Answer: Ix = 4.802 × 10⁶ mm⁴

Composite areas: split the section into rectangles. The centroid is the area-weighted average ȳ = ΣAᵢyᵢ/ΣAᵢ. The second moment of area about the centroidal axis adds each part’s own bh³/12 and its parallel-axis term A·d², where d is the distance from the part’s centroid to the overall centroid. Bending stress is σ = M·y/I.

Split into two rectangles

Measure every y from the bottom edge.

flange: Af = 100·25 = 2500 mm², yf = 100 + 25/2 = 112.5 mm
web: Aw = 14·100 = 1400 mm², yw = 100/2 = 50 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2500·112.5 + 1400·50)/3900 = 90.06 mm

Parallel-axis theorem

flange: 100·25³/12 + 2500·(112.5 − 90.06)² = 1.389 × 10⁶ mm⁴
web: 14·100³/12 + 1400·(50 − 90.06)² = 3.414 × 10⁶ mm⁴
Ix = 1.389 × 10⁶ + 3.414 × 10⁶ = 4.802 × 10⁶ mm⁴ = 4.802 × 10⁶ mm⁴

Answer

Ix = 4.802 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Mallow = 8.915 kN·m

Composite areas: split the section into rectangles. The centroid is the area-weighted average ȳ = ΣAᵢyᵢ/ΣAᵢ. The second moment of area about the centroidal axis adds each part’s own bh³/12 and its parallel-axis term A·d², where d is the distance from the part’s centroid to the overall centroid. Bending stress is σ = M·y/I.

Centroid

ȳ = (5200·270 + 2080·130)/7280 = 230 mm
top edge: c = 280 − 230 = 50 mm

Second moment of area

I = 260·20³/12 + 5200·40² + 8·260³/12 + 2080·100² = 4.101 × 10⁷ mm⁴

Moment allowed by each edge

Sagging: the top is in compression, the bottom in tension.

top edge: M = 120·4.101 × 10⁷/50 = 98.43 kN·m
bottom edge: M = 50·4.101 × 10⁷/230 = 8.915 kN·m

Governing value

Mallow = min = 8.915 kN·m (bottom edge)

Answer

Mallow = 8.915 kN·m

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